Method of compensating a MOS gas sensor, method of manufacturing a MOS gas sensor, MOS gas sensor, and fuel cell system

ABSTRACT

A method of compensating a MOS gas sensor is described and which includes using a MOS gas sensor to provide a signal indicative of gas concentration of a target gas in an ambient; providing a signal representative of dew point of the ambient; and modifying the signal from the MOS gas sensor using the signal representative of dew point to simultaneously compensate for the effects of both temperature and relative humidity on the MOS gas sensor.

TECHNICAL FIELD

The present invention relates to gas sensing instruments, and morespecifically to compensating gas sensors for the effects of ambientconditions such as temperature and humidity. The present invention alsorelates to metal oxide semiconductor sensors utilized as gas sensors.

BACKGROUND OF THE INVENTION

For safety purposes, gas-sensing instruments are used in many industrialapplications such as in fuel cell systems whose feedstocks are flammablegases. It is well known that many gas sensors—metal oxide semiconductor(MOS) based sensors in particular—suffer from environmentaldependencies. That is, ambient temperature and relative humiditysubstantially affect their sensitivity. For example, one commerciallyavailable MOS sensor model is the Figaro TGS821 hydrogen sensor. Due tothe combination of this sensor's environmental dependencies and theenvironmental uncertainties to which it will be exposed to in certainfuel cell applications, a sensor reporting a reading of 526 PPM ofhydrogen might actually be exposed to a true concentration rangingbetween 182 and 1627 PPM. In certain fuel cell applications, the lowerreading would be regarded as being well below alarm-level whereas thehigher reading would be regarded as being well above. This 8.9:1 rangeof uncertainty is the source of much frustration with uncompensated MOSgas sensors.

Accordingly, many designers of gas sensing instruments elect tocompensate for MOS gas sensors'environmental dependencies. Theconventional wisdom is that this requires a microprocessor, firmware(software), and lookup charts. However, dependence upon firmware beingperpetually executed without error in a microprocessor-based circuitgreatly complicates efforts to design a highly reliable, fail-safegas-sensing instrument. Furthermore, the conventional method producescompensation factors that are inexact approximations of the requiredvalues.

Attention is invited to the following U.S. patents, which areincorporated herein by reference: U.S. Pat. No. 5,716,506 to Maclay etal.; U.S. Pat. No. 4,313,338 to Abe et al.; U.S. Pat. No. 4,801,211 toYagi et al.; U.S. Pat. No. 6,126,311 to Schuh; and U.S. Pat. No.5,969,231 to Qu et al.

U.S. Pat. No. 5,716,506 to Maclay et al. discloses (see Col. 1) a gassensor that compensates for relative humidity and temperature of the airin the detection of a predetermined gas in a microfabricatedelectrochemical sensor.

U.S. Pat. No. 4,313,338 to Abe et al. relates to a gas sensing devicecomprising a resistive film formed of ultra fine particles of a metaloxide (Col. 4, lines 10-15). The gas sensing device includes (Col. 7,line 43-Col 8, line 65) a temperature sensing element for maintainingthe temperature of the gas sensitive element constant. U.S. Pat. No.4,313,338 also discloses obviating the problem of water vaporobstructing the successful measurement of the concentration of gas byusing a single gas sensing element to sense both the concentration ofwater vapor and the concentration of isobutane gas (see Col. 8, line47-Col. 9, line 11). The gas sensing element is heated up to 300 degreesCelsius during the measurement of the concentration of the isobutane gasand is cooled down to the room temperature of 25 degrees C. during themeasurement of relative humidity.

U.S. Pat. No. 4,801,211 to Yagi et al. discloses (see Abstract) ahumidity sensor that, when temperature corrected, indicates a dew pointat a fixed temperature. By adjusting this fixed temperature dew pointoutput according to a sensed temperature, the dew point can be detected.FIG. 2 shows analog circuitry employed with same. The sensor isfabricated from metal oxide ceramic material (see Col. 4, lines 44-46).

U.S. Pat. No. 6,126,311 to Schuh discloses (see FIG. 4) a sensor thatoutputs dew point, ambient temperature, and relative humidity. Thispatent discloses (see Col. 1, lines 14-20) that the relative humidityand dew point of a gaseous sample are closely related by well knownalgorithms for converting dew point and ambient temperature to relativehumidity or converting relative humidity and ambient temperature to dewpoint. This patent also indicates (see Col. 2, lines 19-23) that a groupof prior art sensors measure the relative humidity of an ambientenvironment as opposed to dew point, and that relative humidity and dewpoint are easily converted from one to the other with a measurement ofthe ambient air temperature.

U.S. Pat. No. 5,969,231 to Qu et al. discloses a sensor for monitoringthe concentration of moisture and gaseous substances in the air.Semiconductive metal oxides are used (see Col. 1).

Notwithstanding the prior art teachings noted above, none of thesereferences singularly or in any permissible combination teach a simpleapproach for compensating gas sensor measurements for both humidity andtemperature at the same time. It would be advantageous therefore, to beable to perform such compensation utilizing analog circuitry, whichwould be highly reliable and fail safe.

Gas sensors are used, in various industrial applications, such as in thefabrication of fuel cells. For example, gas sensors configured to sensehydrogen can be employed to detect hydrogen fuel leaks or hydrogen fuelflow in the fuel cells. In this regard, attention is directed tocommonly assigned U.S. patent application Ser. No. 09/322,666 filed May28, 1999, listing as inventors Fuglevand et al., and which isincorporated by reference herein. This application discloses theparticulars of how gas sensors can be employed in one form of a fuelcell system.

BRIEF DESCRIPTION OF THE DRAWINGS

Preferred embodiments of the invention are described below withreference to the following accompanying drawings.

FIG. 1 is a perspective, side elevation view of an ion exchange membranefuel cell module which is utilized with a fuel cell power systemembodying the present invention.

FIG. 2 is a perspective, exploded, side elevation view of an ionexchange membrane fuel cell module as seen in FIG. 1.

FIG. 3 is a perspective, partial, exploded, side elevation view of anion exchange membrane fuel cell module as seen in FIG. 1.

FIG. 4 is a fragmentary, perspective, greatly enlarged, exploded view ofa membrane electrode diffusion assembly employed with the ion exchangemembrane fuel cell module as seen in FIG. 1.

FIG. 5 is a fragmentary, side elevational view of a fuel distributionassembly utilized with the ion exchange membrane fuel cell module asseen in FIG. 1.

FIG. 6 is a second, fragmentary, side elevational view of the fueldistribution assembly taken from a position opposite to that seen inFIG. 5.

FIG. 7 is a second, perspective, partial, exploded view of a portion ofthe ion exchange membrane fuel cell module as seen in FIG. 1.

FIG. 8 is a perspective view of an ion exchange membrane fuel cellsubrack and associated fuel gas supply.

FIG. 9 is a fragmentary, transverse, vertical sectional view taken froma position along line 9—9 of FIG. 8.

FIG. 10 is a fragmentary, schematic representation of an ion exchangemembrane fuel cell module, and associated power system.

FIG. 11 is a graph illustrating the average ratiometeric response of atypical MOS gas sensor to the concentration of a gas used as a fuel inthe fuel cell system as illustrated.

FIG. 12 is a graph illustrating the effects of temperature and humidityon the same MOS gas sensor.

FIG. 13 is a graph illustrating dew points plotted against Rs/Ro valuesfor the same MOS sensor.

FIG. 14 is a graph illustrating environmental Rs/Ro relationships usingdew points for the same MOS gas sensor.

FIG. 15 is a graph illustrating the relationship of compensation factorsvs. water content for the same MOS gas sensor.

FIG. 16 is a block diagram illustrating the circuitry utilized totransform a dew point signal into a linear or semi-linear compensationfactor and multiply that same compensation factor by the output of theMOS gas sensor.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

This disclosure of the invention is submitted in furtherance of theconstitutional purposes of the U.S. Patent Laws “to promote the progressof science and useful arts” (Article 1, Section 8).

The present invention provides for a method of compensating a MOS gassensor, comprising using a MOS gas sensor to provide a signal indicativeof gas concentration of a target gas in an ambient; providing a signalrepresentative of dew point of the ambient; and modifying the signalfrom the MOS gas sensor using the signal representative of dew point tosimultaneously compensate for the effects of both temperature andrelative humidity on the MOS gas sensor.

Another aspect of the present invention provides for a method ofcompensating a MOS gas sensor, comprising: utilizing a MOS gas sensor,providing a signal indicative of gas concentration of a target gas in anambient; determining the dew point of the ambient; determining acompensation factor for the MOS gas sensor, the compensation factorbeing determined based upon the ascertained dew point; and modifying theresulting signal from the MOS gas sensor using the compensation factor.

Another aspect of the present invention provides for a MOS gas sensorsystem comprising a MOS gas sensor configured to provide a signalindicative of gas concentration of a target gas in an ambient; equipmentconfigured to determine the dew point of the ambient; and compensationcircuitry configured to modify the signal from the MOS gas sensor usinga compensation factor, the compensation factor being selected based onthe determined dew point.

Another aspect of the present invention provides for a method ofmanufacturing a MOS gas sensor system, comprising: providing a MOS gassensor of a particular model, the MOS gas sensor providing a signalindicative of gas concentration of a target gas in an ambient;determining a compensation factor for the MOS gas sensor selected, andresponsive to dew point; and providing analog circuitry configured tomodify the signal from the MOS gas sensor using the compensation factor.

Yet another aspect of the present invention provides for a fuel cellsystem comprising a housing having a fuel gas inlet and an exhaustoutlet; at least one ion exchange fuel cell membrane located within thehousing, and wherein the ion exchange membrane has opposite sides; ananode electrode mounted on one side of the ion exchange fuel cellmembrane, and a cathode electrode mounted on the opposite side of theion exchange fuel cell membrane; and a MOS gas sensor system including aMOS gas sensor which senses the presence of a fuel in the housing, andwhich provides a signal indicative of the gas concentration of the fuelin the housing; equipment configured to determine the dew point in thehousing; and circuitry configured to modify the signal from the MOS gassensor using a compensation factor which is selected based upon thedetermined dew point.

Another aspect of the invention provides a method of compensating asignal from a MOS gas sensor, comprising compensating the signal fromthe given MOS sensor for the effects of dew point by using a firstformula w′=((Log(Rcomp/Ro)+2α)/α) where w′ is compensated gasconcentration in parts per million, where Ro is resistance in ohms forthe given MOS gas sensor at 100 PPM when measured at a dew pointcompensation factor K of unity, where a represents the sensitivity ofthe given MOS gas sensor, and by using a second formulaRcomp=10{circumflex over ( )}(Log(Rs)+(Log(K)/Ka)α) where Rs is theoutput of the given sensor, in ohms, indicative of hydrogen gasconcentration when influenced by the effects of dew point, where K is alive variable that, when multiplied by the output of the given sensor,compensates for the effects of dew point, and where Ka is a constanthaving the fixed value of α for which K factors were optimized and whichscales the effect of K factor depending on the sensitivity (α) of thegiven sensor.

As best seen in FIG. 8, an ion exchange membrane fuel cell power system10 is made up of a plurality of fuel cell modules 11, one of which isshown in FIG. 1. The ion exchange membrane fuel cell power system 10 mayinclude a plurality of subsystems or subracks 210. As illustrated eachsubsystem or subrack 210 includes a plurality of hand manipulablemodules 11 (FIG. 1) which respectively have a forward edge 12, anopposite, rearward edge 13, top and bottom surfaces or edges 14 and 15,and opposite sidewalls generally indicated by the numeral 16. Each facetof the module 11 will be discussed in greater detail hereinafter. Yetfurther those should recognize that the present invention could beemployed with conventional stack-like technology wherein the individualsubsystem comprises fuel cell stacks arranged in a manner which isconsistent with the further teachings of this application.

As best seen in FIGS. 2 and 3, the fuel cell module 11 includes anonconductive, dielectric support member generally indicated by thenumeral 20. The support member can be fashioned out of various syntheticpolymeric substrates. The support member has (see FIG. 3) a main body21, which is defined by a forward peripheral edge 22; a rearwardperipheral edge 23; a top peripheral edge 24; an opposite, bottomperipheral edge 25; and opposite sidewalls generally indicated by thenumeral 26.

As best seen in FIG. 2, a pair of recessed channels 30 are formed in theforward peripheral edge 22. Further, a plurality of fastener receivingpassageways or apertures 31 are also formed in the forward peripheraledge 22. Yet further, and as seen in FIG. 3, a plurality of spaced ribs32 are borne by, or made integral with the respective sidewalls 26 andare disposed in spaced relation, one to the other. Fastener passagewaysor apertures 33 are formed through each of the ribs. Further, cavities34 are defined between the respective ribs 32 on each sidewall. Thecavities 34 formed on each of the sidewalls are disposed insubstantially opposed relation one to the other. This is seen in FIG. 3.

Further, as best seen in FIG. 3, orientation members 35 are disposedbetween each of the ribs 32 and define a space therebetween. A pair ofmounting tabs 36 are provided in spaced relationship, one to the other,on the rearward peripheral edge 23 of the main body 21. A pair ofsubstantially coaxially aligned apertures 37 are individually formed ineach of the mounting tabs 36 and are operable to receive a fastenertherethrough.

A fuel coupling 40 is made integral with or forms a portion of therearward peripheral edge 23 of the support member 20. The fuel coupling40 includes a fuel delivery passageway 41 which is substantially Tshaped and which is defined by an intake end 42 and a pair of exhaustends labeled 43. Additionally, the fuel coupling also includes anexhaust passageway 44 which is also substantially T shaped and which isdefined by a pair of intake ends 45, and an exhaust end 46. Theoperation of the fuel coupling 40 will be discussed in greater detailhereinafter.

As best seen in FIGS. 2 and 3, individual conductor plates generallydesignated by the numeral 50 are matingly received within the individualcavities 34 which are defined by the support member 20. The conductorplates which are fabricated from an electrically conductive substrate,have a substantially planar main body 51, which has a first end 52, andan opposite, second end 53. The main body 51 further has a conductivetab 54 which extends outwardly relative to the first end 52, and whichis oriented between the individual orientation members 35. Theconductive tab extends substantially normally outwardly relative to thetop peripheral edge 24 of the support member 20. As will be recognized,the main body 51 matingly rests between the individual ribs 32 whichdefine, in part, the respective cavities 34.

As best seen in the exploded view of FIG. 3, a cathode current collectoris generally designated by the numeral 60, and rests in ohmic electricalcontact with the main body 51 of the individual conductor plates 50. Thecathode current collector, which is fabricated from an electricallyconductive substrate, has a main body 61 which has opposite first andsecond ends 62 and 63, respectively. The cathode current collectorsimultaneously performs the functions of current collection, forceapplication and heat dissipation. Still further, the main body 61 of thecurrent collector 60 is defined by a peripheral edge 64.

As best seen in the exploded view of FIGS. 4 and 7, the ion exchangemembrane fuel cell module 11 includes a plurality of membrane electrodediffusion assemblies generally indicated by the numeral 100. Each of themembrane electrode diffusion assemblies have an anode side 101, and anopposite cathode side 102. Still further, each of the membrane electrodediffusion assemblies is defined by a peripheral edge 103, and furtherhas formed in its anode side, a plurality of interlinking channels 104.The membrane electrode diffusion assembly 100, as noted above, is formedof a solid ion conducting membrane 105 which is sealably mounted orreceived in each of the respective cavities 34. In this arrangement, thecathode side 102 of each membrane electrode diffusion assembly 100 isheld in spaced relation relative to the support member 20 by deformableelectrically conductive members 70 (FIGS. 2 and 3) of the cathodecurrent collector 60. This spacial arrangement, which is provided by thecathode current collector, facilitates, in part heat dissipation fromthe fuel cell module 11. As described, above, the membrane electrodediffusion assembly 100; associated cathode current collector 60; andsupport member 20 in combination, define a cathode air passageway 106therebetween (FIG. 10). The construction of a suitable membraneelectrode diffusion assembly was described in our earlier U.S. Pat. No.6,030,718. This earlier patent is incorporated by reference herein, andfurther discussion regarding the construction of the membrane electrodediffusion assembly is not undertaken herein.

As will be appreciated, from a study of FIG. 10, the cathode airpassageway 106 is defined or otherwise oriented on each side 26 of thesupport member 20. Therefore, the fuel cell module 11 has a bifurcatedcathode air flow. As will be appreciated, while the earlier describedmembrane electrode diffusion assembly was directed to a proton exchangemembrane, the fuel cell power system 10 is not limited solely to a typehaving proton exchange membranes, but also may utilize anion exchangemembranes.

As best seen by reference to FIGS. 5, 6 and 7, a fuel distributionassembly, which is generally indicated by the numeral 110, is coupled influid flowing relation relative to the anode side 101 of each of themembrane electrode diffusion assemblies 100. Each fuel distributionassembly 110 is coupled with a source of a fuel 340 (FIG. 8) which maybe substantially pure, or which is diluted to various degrees. Such maybe achieved if the fuel cell power system was coupled with a fuelprocessor which would produce a stream of hydrogen from a source ofhydrocarbon fuel such as gasoline, natural gas, propane, etc. If thefuel cell power system 10 was fabricated in the nature of a protonexchange membrane fuel cell, the dilute fuel supply would includehydrogen. The concentration of the hydrogen in the dilute fuel wouldnormally be in a range of about 30% to about 80% by volume.

When supplied with this dilute fuel mixture (regardless of the type),the fuel cell modules 11 produce an average current density of at leastabout 350 mA per square centimeter of surface area of each anode side101 at a nominal voltage of 0.5 volts. Further, the interlinkingchannels 104 formed in the surface of the anode side 101 facilitate thedistribution of the dilute fuel substantially about the entire surfacearea of the anode side 101. In this arrangement, if contaminants areintroduced by way of the dilute fuel mixture or other blockage occurs,the interlinking channels 104 provide a convenient passage by which thefuel may reach substantially the entire surface area of the anode side101, even though some portions of the interlinking channels 104 may beblocked or otherwise substantially occluded. As noted above, the dilutefuel 340 may be supplied by a fuel processor 342 (FIG. 8) which receivesa hydrocarbon based fuel, and then through a chemical reactionfractionates the hydrocarbon fuel source to liberate a dilute stream ofhydrogen which is mixed with other substances. In the alternative, thefuel may be supplied by a pressurized container 341. These alternativearrangements are shown in FIG. 8.

As best seen by reference to the exploded view as shown in FIG. 7 andFIG. 1, the ion exchange membrane fuel cell module of the presentinvention includes a pair of the fuel distribution assemblies 110 whichare individually mounted in fluid flowing relation relative to the anodeside 101 of the respective membrane electrode diffusion assemblies 100.

As best seen in FIGS. 5 and 6, each of the fuel distribution assemblies110 include a main body 111 which has an inside facing surface 112,(FIG. 6) and an outside facing surface 113 (FIG. 5). The main body 111further defines an intake plenum 114, and an exhaust plenum 115.Further, a fluid coupling 116 (FIG. 1) is mounted in fluid flowingrelation relative to the individual intake and exhaust plenums 114 and115 respectively. A reduced dimension orifice 114 a (FIG. 5) is formedin the main body and communicates with the intake plenum 114. Thisreduced diameter orifice operates to create a pressure differential inthe respective apertures or cavities 120 during certain operationalconditions to facilitate the clearance of contaminants or otherobstructions which may be blocking any of the channels 104 which areformed in the membrane electrode diffusion assembly 100. A plurality ofcavities or apertures 120 are formed in the main body 111, and extendbetween the inside and outside facing surfaces 112 and 113 respectively.The cavities or apertures 120 are disposed in spaced relation, one tothe other, and when assembled, the cavities 120 receive the individualmembrane electrode diffusion assemblies 100. As best seen in FIG. 5, aplurality of channels or passageways 121 are formed in the main body111, and couple the individual cavities 120 in fluid flowing relationwith the respective intake and exhaust plenums 114 and 115.Additionally, a plurality of fastener apertures 109 are formed in themain body. As further seen in FIG. 7, a sealing member 122 lies incovering relation relative to the individual channels 121.

As best seen in FIG. 1, a plurality of conduits 150 couple in fluidflowing relation the fuel coupling 40 with the fuel distributionassembly 110. Two of the conduits designated as 151 allow a dilute fuelmixture to be delivered by way of the intake plenum 114 to theindividual membrane electrode diffusion assemblies 100. Thereafter, anyremaining fuel, and associated by-products of the chemical reaction arereceived back into the exhaust plenum 115 and then flow by way ofconduits 152 to the fuel coupling 40 and then to the exhaust passageway44.

First and second pressure sensitive adhesive seals 123 and 124 (FIG. 7),respectively are provided, and are disposed in juxtaposed relationrelative to the opposite inside and outside facing surfaces 112 and 113respectively. Each of the seals 123 and 124 have apertures 125 formedtherein which are substantially coaxially oriented relative to therespective cavities 120. As will be recognized, the cavities 120 whichare formed in the main body 111 of the fuel distribution assembly 110,matingly cooperate and are substantially coaxially aligned with theindividual cavities 34 which are formed in the nonconductive supportplate 20. As will be recognized and following the assembly of same, therespective membrane electrode diffusion assemblies 100 are individuallyreceived in mating relation in each of the cavities 120 and 34 which aredefined by both the fuel distribution assembly 110, and the supportmember 20. Further, a plurality of fastener apertures 126 are formed inthe individual seals 123, and 124, and are operable to receive fastenerswhich will be discussed in greater detail hereinafter.

Lying in immediate juxtaposed relation relative to the second pressuresensitive adhesive seal 124 is an anode current collector which isgenerally designated by the numeral 140. Additionally, and as seen inFIG. 7, a substantially rigid sealing plate 130 is provided and which isjuxtaposed relative to the cathode side 102 of the membrane diffusionassembly 100. The sealing plate 130 has a main body 131 which defines aplurality of apertures 132 which matingly receive, in part, therespective membrane electrode diffusion assemblies 100. Still further,the main body has a plurality of fastener apertures 133 formed thereinand which when assembled, are substantially coaxially aligned with theaforementioned fastener apertures formed in the earlier describedportions of the fuel cell module 11.

Each anode current collector 140 lies in ohmic electrical contactagainst the anode side 101 of each of the membrane electrode diffusionassemblies 100 and further is oriented in heat receiving relationrelative thereto. The anode current collector 140 has an electricallyconductive main body 141 which has an inside facing surface 142 whichlies against the anode side 101 of the membrane electrode diffusionassembly 100, and an opposite outside facing surface 143. Still further,a plurality of fastener apertures 144 are formed in the main body 131and are operable to be substantially coaxially aligned relative to theother fastener apertures 126 formed in the various seals 123, 124, andin the fuel distribution assembly 110.

As seen in FIG. 7, an electrically insulative member or gasket 160 ismounted or oriented in juxtaposed relation relative to the outsidefacing surface 143 of the anode current collector 140. This insulativemember has a main body 161 which has an inside facing surface 162 whichrests in contact with the outside facing surface 143 of the anodecurrent collector, and further has an outside facing surface 163.Further, a plurality of fastener apertures 164 are operable to becoaxially aligned with the previously described fastener aperturesformed in the remaining parts of the ion exchange membrane fuel cellpower system 10.

As best seen in FIG. 7, an anode heat sink 170 is oriented in juxtaposedrelation relative to the insulative member 160, and further, is mountedin heat receiving relation relative to the anode sides 101 of each ofthe membrane electrode diffusion assemblies 100 to conduct heat energygenerated by the ion exchange membrane module 11 away from the membraneelectrode diffusion assembly 100. In this arrangement, the fueldistribution assembly 110 is located substantially between the anodeside 101 of the membrane electrode diffusion assembly 100, and the anodecurrent collector 140. The anode heat sink 170 has a main body 171 whichhas an inside facing surface 172, which lies in juxtaposed relationrelative to the insulative member 160, and an opposite outside facingsurface 173. Similarly, and as discussed above, numerous fastenerapertures 174 are formed therein, and which are substantially coaxiallyaligned with the remaining fastener apertures which are formed in theearlier disclosed portions of the ion exchange membrane fuel cell module11. Fasteners 175 are provided and are received in these coaxiallyaligned fastener apertures such that the module is held firmly together.These fasteners 175 along with the respective current collectors 60create sufficient pressure to allow the individual current collectors 60and 140 to make effective ohmic electrical contact with the anode andcathode sides 101 and 102, respectively, of the membrane electrodediffusion assembly 100. As will be recognized from the discussion above,the anode current collector 140 is substantially electrically isolatedfrom the anode heat sink 170. Additionally, the anode heat sink hassufficient thermal conductivity such that it substantially inhibits theformation of a temperature gradient across the membrane electrodediffusion assembly 100 during operation of the ion exchange membranefuel cell power system 10.

A handle assembly is generally indicated by the numeral 190 and is bestseen in FIG. 2. As shown therein, the handle assembly 190 has a backplate generally indicated by the numeral 191, and which is defined by afront surface 192, and an opposite rear surface 193. Formed through thefront and rear surfaces is an aperture 194 which matingly receives themember 84 which is mounted on the main body 81 of the current conductorassembly 80. Still further, a pair of handles 195 are fastened on thefront surface 192, and additionally, a plurality of fastening apertures196 are formed through the front and rear surfaces 192 and 193 and areoperable to receive fasteners 197 which threadably engage the fastenerapertures 31, which are formed in the forward edge 23 of the supportmember 20. The handles permit the module 11 to be easily manipulated byhand, and removed without the use of any tools, when utilized with asubrack or sub-system which will be discussed in greater detailhereinafter.

The ion exchange membrane fuel cell module 11 is employed in combinationwith a plurality of subracks or sub-systems 210, one of which is shownin FIGS. 8 and 9 and which is generally indicated by the numeral 210.Each subrack 210 releasably supports a plurality of ion exchangemembrane fuel cell modules 11 in an operable arrangement. Each subrack210 includes a principal enclosure 211. The principal enclosure isdefined by a top surface 212; bottom surface 213; front sidewall 214;rear sidewall 215; left sidewall 216, and right sidewall 217. Therespective sidewalls 212 through 217 define an internal cavity 220 (FIG.9). In this arrangement, the principal enclosure will receive multiplefuel cell modules 11, each enclosing a membrane electrode diffusionassembly 100.

As seen in FIG. 8, the ion exchange membrane fuel cell power system isconfigured in a manner where at least one of the fuel cell modules 11can be easily removed from at least one of the subracks 210 by hand,while the remaining modules continue to operate. As noted above thisremoval is normally accomplished without the use of any tools, howeverit may be necessary in some commercial or industrial applications wherevibration, and other outside physical forces may be imparted to thesystem, to use threaded fasteners and the like to releasably secure theindividual modules to the subrack 210 to prevent the unintentionaldisplacement or dislocation of the respective modules from the subrack210. If utilized, the hand tools which will be employed will be simplehand tools, and the removal will be accomplished in minutes, as opposedthe prior art stack arrangements where replacement of a damaged membraneelectrode assembly (MEA) may take hours to accomplish. It should beunderstood that the terms “subrack” and “sub-system” as used in thefollowing claims do not necessarily imply that a rack or shelf isrequired, only that the sub-system, or a portion thereof, is operableindependently whether or not other sub-system, or a portion thereof, ofthe fuel cell power system 10 are functioning.

As best seen by reference to FIG. 9, an aperture 230 is formed in thetop surface 12 of the subrack 210, and further, the cavity 220 iscomprised of a first or fuel cell module cavity 231, and a second cavityor electrical control bay 232. As best seen by reference to FIG. 8, aplurality of individual module apertures 233 are formed in the frontsurface 214 of the principal housing 211, and are operable toindividually receive the respective fuel cell modules 11, and positionthem in predetermined spaced relation, one to the other.

The fuel cell module cavity 231 is further defined by a supportingmember or shelf 234 (FIG. 9) which orients the individual fuel cellmodules 11 in a predetermined substantially upright orientation withinthe cavity 231. Additionally, the fuel cell module cavity 231 is definedby a rear wall 235 which supports a DC bus 236 in an orientation whichwill allow it to releasably, matingly, electrically couple with thecurrent conductor assembly 80 (FIG. 2) which is borne by the fuel cellmodule 11. Yet further, and as seen in the cross sectional view of FIG.9, the rear wall 235 further supports a fuel supply line 237 and abyproduct removal line 238. These are operable to be releasably coupledin fluid flowing relation with respect to the fuel delivery passageway41 and the exhaust passageway 44 of the fuel coupling 40.

As best seen in FIG. 9, the second cavity or electrical control bay 232encloses a digital or analog controller 250 which is electricallycoupled with the respective ion exchange membrane fuel cell modules 11,and a power conditioning assembly 260 which is electrically coupled withthe DC bus 236, and the controller 250, and which is operable to receivethe electrical power produced by the ion exchange membrane fuel cellmodules 11. The operation of the controller 250 and power conditioningassembly 260 and related control circuitry is discussed in prior U.S.application Ser. Nos. 09/108,667 and 09/322,666, which are incorporatedby reference herein.

As further seen in FIG. 9, an aperture 270 is formed in the rear wall215 of the principal enclosure 211, and is operable to receive an airfilter 271 which is operable to remove particulate matter from anoutside ambient air stream passing therethrough and into the principalenclosure 211.

As best seen by the cross sectional view in FIG. 9, the subrack 210includes an air distribution plenum 290 which is coupled in fluidflowing relation relative to each of the ion exchange membrane fuel cellmodules 11. The air distribution plenum 290 has a first or intake end291 which receives both air which has previously come into contact witheach of the ion exchange fuel cell modules 11, and air which comes fromoutside of the respective ion exchange membrane fuel cell modules.Further, the air distribution plenum has a second or exhaust end 292which delivers an air stream to each of the ion exchange fuel cellmodules 11. Disposed intermediate the first or intake end 291, and thesecond or exhaust end 292 is an air mixing valve 293 which is coupled tothe air distribution plenum 290, and which meters the amount of airwhich is passed through the respective ion exchange membrane fuel cellmodules 11 and is recirculated back to the ion exchange fuel cellmembrane modules and by way of the air filter 271. As illustrated, themixing valve 293 selectively occludes an aperture 294 which is formed inthe rear wall 215 of the subrack 210.

An air movement assembly such as a fan 295 is provided and is mountedalong the air distribution plenum 290. As shown in FIG. 9, the airmovement assembly 295 is positioned near the intake end 291, and issubstantially coaxially aligned with the aperture 230 which is formed inthe top surface 212 of the subrack 210. The air mixing valve and the fanassembly 293 and 295 respectively are electrically coupled with thecontroller 250 and are controlled thereby. The air mixing valve 293comprises a pivotally movable valve member 296 which can be moved from afirst occluding position 297 relative to the aperture 294, and a second,substantially non-occluding position 298 as shown in phantom lines.

As will be recognized, when the valve member 296 is in the secondnon-occluding position, air received in the intake end 291 and which haspreviously passed through the individual fuel cell modules will pass outof the principal enclosure 211 and then be exhausted to the ambientenvironment. On the other hand, when the valve member 296 is in theoccluding position 297 air from the intake end 291 which has passedthrough the fuel cell module 11 will return to the exhaust end and thenpass through the modules 11 and return again to the intake end. As willbe recognized, by controlling the relative position of the valve member296, temperature as well as relative humidity of air stream 299 can beeasily controlled. Still further, in the occluding position 297, airfrom the ambient will continue to enter the air distribution plenum byway of the air filter 270.

More specifically, the air stream 299 which is supplied to the fuel cellmodules is provided in an amount of at least about 5 to about 1000 timesthe volume required to support a fuel cell chemical relation whichproduces water vapor as a byproduct. The present air plenum arrangementprovides a convenient way by which the air stream delivered to thecathode side 102 can be humidified by the water vapor generated as abyproduct of the chemical reaction taking place on the cathode.Additionally, during cold operating conditions, this same air, which hasnow been heated by each of the fuel cell modules 11, will contribute tobringing the entire fuel cell up to normal operating temperatures.Further, the air mixing valve 293 limits the amount of air which haspreviously passed through the modules 11 and which is added to the airdistribution plenum 290. This resulting recirculated air stream andfresh ambient air forms an air stream having substantially optimaloperating characteristics which maximizes the current densities andoutputs of the respective membrane electrode diffusion assembliesenclosed within each of the fuel cell modules 11.

Referring now to FIG. 10, what is shown is a greatly simplified,exaggerated, partial, and cross-sectional view of an ion exchangemembrane fuel cell module 11 positioned in an operational relationshiprelative to the air distribution plenum 290. This particular sectionalview, which does not include many of the subassemblies previouslydiscussed, is provided to illustrate the principals that will be setforth below. As seen in FIGS. 9 and 10, and as discussed above, thesubrack 210 includes an air distribution plenum 290 which provides astream of air 299 to each of the ion exchange fuel cell modules 11 whichare received in an operational position on the shelf or supportingmember 234. The air stream 299 exits from the exhaust end 292 and thenbecomes a bifurcated air flow which is generally indicated by thenumeral 320. The bifurcated air flow 322 comprises a first cathode airstream 321, which is received in the respective ion exchange membranefuel cell modules 11; and a second anode heat sink air stream which isgenerally indicated by the numeral 322. As will be recognized by a studyof FIG. 10, the first cathode air stream 321 enters the ion exchangemembrane fuel cell module 11, and is further bifurcated into a firstcomponent 323 which moves along one of the cathode air passageways 106which is defined on one side of the support member 20. Further, thefirst cathode air stream 321 has a second component 324 which passesalong the cathode air passageway 106 on the opposite side of the supportmember 20. As will be appreciated, the bifurcated cathode air stream 321provides the necessary oxidant (oxygen in the ambient air stream) to thecathode side 102 of the membrane electrode diffusion assembly 100. Yetfurther, the cathode air flow operates to remove less than apreponderance of the heat energy generated by the membrane electrodediffusion assembly 100 while it is in operation. As will be recognizedthe cathode air flow is facilitated by the respective cathode currentcollectors 60 which create in part, the cathode air passageway 106.

The anode heat sink air stream 322 is further bifurcated into a firstcomponent 325 and a second component 326, both of which individuallymove along the opposite sides 16 of the ion exchange membrane fuel cellmodule 11, and over each of the anode heat sinks 170. As the anode heatsink air stream components 325 and 326 move over the opposite anode heatsinks 170, the anode heat sink air stream operates to remove apreponderance of the heat energy generated by the ion exchange membranefuel cell module 11 during operation. Therefore, it will be recognizedthat the present invention provides an ion exchange fuel cell module 11which has a bifurcated air flow 320 which regulates the operationaltemperature of the ion exchange membrane fuel cell module by removingthe heat energy generated therefrom.

Referring now to FIG. 8, and as earlier discussed, the individual ionexchange membrane fuel cell modules 11 and the subrack 210 comprise incombination a fuel cell power system which is coupled in fluid flowingrelation relative to a source of a substantially pure or dilute fuelgenerally indicated by the numeral 340. The fuel gas supply may comprisea source of bottled and compressed fuel gas generally indicated by thenumeral 341, or a fuel stream which is provided by a chemical reactor,or fuel processor 342 which produces the fuel stream for use by theindividual ion exchange fuel cell modules 11. A conduit 343 coupleseither fuel gas supply 340 with the respective ion exchange fuel cellmodules 11 and the associated subrack 210. When a chemical fuelprocessor 342 is provided, the fuel processor would receive a suitablehydrocarbon fuel stream such as natural gas, propane, butane, and otherfuel gases and would thereafter, through a chemical reaction release afuel stream which would then be delivered by way of the conduits 343.

The present fuel cell power system 10 may also include a fuel gasrecovery and recycling system (not shown) which would recover orrecapture unreacted fuel gas which has previously passed through theindividual ion exchange fuel cell modules 11. This system, in summary,would separate the unreacted fuel gas and would return the unreactedfuel gas back to the individual ion exchange fuel cell modules forfurther use. This recovery system would be coupled with the byproductremoval line 238.

Although a certain number of subracks 210 are shown in the drawings, anda certain number of fuel cell modules 11 are shown per subrack 210, itwill be readily apparent that any desired number of subracks and modules11, or a portion thereof, could be employed in alternative embodiments.

The fuel cell power system 10 (FIG. 9) includes one or more gas sensors400 in one or more locations and which are used, for example, to detectthe presence of fuel (e.g., hydrogen gas). The presence of hydrogen gasin certain areas of the fuel cell power system 10 of the subracks 210may indicate a fuel leak. Such fuel leaks can be potentially hazardousunder certain operating conditions. One such sensor 400 is shown in FIG.9. The sensor 400 has a sampling port 403, including a sensor element,and a baffle protecting the sensor element; e.g., from high velocityairflow. The sampling port 403 is the part of the sensor primarilyexposed to the target gas. In one embodiment, the baffle comprises asintered bronze disk. Other alternatives could be employed. For example,the baffle could just as easily be a piece of chemist's filter paper.Further, if the sampling port 403 is located in an area that does nothave ventilation or high airflow, the baffle is not necessary and can beomitted altogether.

The sensor 400 includes a heater for heating the sensor element to apredetermined operating temperature. The heater can be, for example, awire that is spirally wound relative to the sensor element. Such heatersprovide heat in a predefined temperature range to assure properoperation of the accompanying sensor. Other configurations are, ofcourse, possible for the sensor 400. In operation, an electrical currentis applied to the heater associated with the sensor 400, at apredetermined power level, to maintain the element at a specifiedoperational temperature. For example, with one commercially availablesensor, approximately 600 mW of power maintains the sensor at atemperature of 500° C.

The fuel cell power system 10 further includes circuitry 402 which iselectrically coupled to the sensor 400. The circuitry 402 controlsoperation of the sensor 400 (e.g. generation of heat by the heaterincluded in the sensor 400) and further is coupled to the controller250. In one embodiment, the circuitry 402 is a printed circuit cardassociated with the sensor 400 and which is provided by the manufacturerthereof.

In one embodiment, for example (see FIG. 9), the gas sensor 400 ispositioned such that it may sense hydrogen gas in the plenum 290. Inthis embodiment, the gas sensor 400 is primarily housed in the cavity orelectrical control bay 232. The circuitry 402 associated with the card(discussed above) is also located in the electrical control bay 232 andis mounted, for example, on ¼-inch-long standoffs which are affixed tothe top of the control bay 232. As seen in FIG. 9, the sampling portdisk 403 protrudes through the bulkhead 405 separating the chamber 232and the plenum 290 in order to position the sampling port 403 insideplenum 290.

Other locations for the sensor 400 are, of course, possible. Thelocation is, in the illustrated embodiment, selected such that thesampling port 403 is positioned downstream of the fan 295. This locationinsures that leaking hydrogen is homogenized into the air, but isdetected before encountering any mixing vanes 293, or where fresh air isintroduced 271. Further, the location, in the illustrated embodiment, isselected such that the circuitry 402 and the electrical connectorbetween the circuitry 402 and the sensor 400 are located within thecontrol bay 232 so that this connector does not have to pierce thebulkhead 405. This also allows the electronics of the circuitry 402 tobe located in an area that is cooled via fan-forced air.

Alternatively, the sensor 400 may be located in the plenum 290 and theelectrical connector between the circuitry 402 and the sensor 400 mustthen pierce the bulkhead 405. This is less desirable because the fuelcell system 10 circulates air at about 55 degrees C. and this highertemperature lessens the life of power-producing electronic components onthe circuitry 402. Further, a seal is required where the cable piercesthe bulkhead 405.

The fuel cell power system 10 further includes dew point determiningequipment 401. In one embodiment of the invention, the dew pointdetermining equipment comprises chilled-mirror equipment, configured toprovide a signal representative of the dew point. Chilled-mirror dewpoint determining equipment is described, in greater detail, in thefollowing U.S. patents which are incorporated herein by reference: U.S.Pat. No. 5,739,416 to Hoenk; U.S. Pat. No. 5,507,175 to Cooper; and U.S.Pat. No. 6,155,098 to Shapiro et al. In an alternative embodiment, thedew point determining equipment comprises a temperature sensor and arelative humidity sensor.

The fuel cell power system 10 further includes conditioning circuitry402 which is electrically coupled to the sensor 400 and to the dew pointdetermining equipment 401, for reasons that will be described in greaterdetail below. In this regard, the conditioning circuitry 402 conditionsthe output signal of the sensor 400 and provides the conditioned signalto the controller 250.

While other sensors could be employed, in the illustrated embodiment,the sensor 400 is a metal oxide semiconductor (MOS) hydrogen sensor,model TGS 821, and which is commercially available from FigaroEngineering (Figaro). Figaro's sensors are described in the followingU.S. patents, which are incorporated herein by reference: U.S. Pat. No.5,006,828 to Yutaka et al.; U.S. Pat. No. 4,958,513 to Yasunga et al.;U.S. Pat. No. 4,938,928 to Koda et al.; U.S. Pat. No. 4,827,154 toNaoyuki et al.; U.S. Pat. No. 4,816,800 to Onaga et al.; U.S. Pat. No.4,731,226 to Takahata et al.; U.S. Pat. No. 4,718,991 to Yamazoe et al.;U.S. Pat. No. 4,701,739 to Sasaki; U.S. Pat. No. 4,658,632 to Sasaki;U.S. Pat. No. 4,575,441 to Murakami et al.; U.S. Pat. No. 4,459,577 toMurakami et al.; and U.S. Pat. No. 4,117,082 to Matsuyama.

FIG. 11 illustrates temperature/humidity dependency. More particularly,FIG. 11 shows the average ratiometric response of one sensor model, theFigaro TGS821, to hydrogen and shows environmental offsets. Therelationship between hydrogen concentration versus relative resistance,at an environmental dependency Rs/Ro of unity (where the effects due totemperature and relative humidity are null), can be described by aformula of the form y=mx+b and is given by the function y=10{circumflexover ( )}(αLog(w)−2α). Here, “y” is the Rs/Ro ratio and is the sensor'ssensitivity ratio normalized to unity at a gas concentration of 100 PPM.The term “w” is the hydrogen gas concentration in PPM. The term “α”(alpha) describes the sensor's sensitivity slope (how steep it is).Whereas a for one particular sensor (Figaro TGS821) averages −0.725,manufacturing tolerances are such that a ranges from −0.6 to −1.2. Theactual sensor resistance for any given hydrogen concentration at anenvironmental dependency Rs/Ro of unity, is given by the formulaR=10{circumflex over ( )}(3.5±0.5)y. The term “R” is sensor resistance(Ω) and the term “y” is the sensor's sensitivity Rs/Ro ratio. This meansthat at an environmental dependency Rs/Ro ratio of unity, the averagesensor of this model has about 3.2 kΩ of resistance at 100 PPM, butranges from 1.0 kΩ to 10 kΩ). As can be seen, the sensitivity of thesensor defined by the relationship between gas concentration changes andthe sensor resistance changes is based on a logarithmic function. Thex-axis is gas concentration and the y-axis is indicated as a sensorresistance ratio Rs/Ro where Rs is sensor resistance. In the graph ofFIG. 11, the four slopes 408, 410, 412, 414 adjacent to the main (bold)one 406 denote the extent to which temperature and relativehumidity—environmental dependencies—can affect the sensor's signaloutput in fuel cell applications. Slope 406 is an environmentaldependency Rs/Ro of unity, slope 408 is an environmental dependencyRs/Ro of 0.8, slope 410 is an environmental dependency Rs/Ro of 0.6835,slope 412 is an environmental dependency Rs/Ro of 1.25, and slope 414 isan environmental dependency Rs/Ro of 1.5109.

Note the error bar 500 on FIG. 11. Without circuitry to compensate forthe environmental effects to which fuel cells are subjected, orknowledge of the environmental circumstances, a reported reading of 545PPM could reside anywhere on the line segment 502 projecting to theright from the bottom of the error bar 500 (at an Rs/Ro ratio of 0.200)and the true concentration could be as great as 1627 PPM. Just aseasily, a reported reading of 545 PPM could reside anywhere on the linesegment 504 projecting to the left from the top of the error bar (at anRs/Ro ratio of 0.442) and the true concentration could be as little as182 PPM. This is an 8.9:1 range of uncertainty and is the source of muchfrustration with uncompensated MOS gas sensors.

It may also be advantageous to have circuitry associated with a sensor,such as circuitry 402 in the present embodiment, be of an all-analogdesign (i.e., a design with no microprocessor at the heart of the devicecontinually running firmware or software) in certain embodiments. Itshould be appreciated that in certain safety-critical applications, itcan be very challenging to design both fail-safe microprocessor-basedhardware and fail-safe firmware. Yet further, It can be even morechallenging—and costly—to prove to nationally recognized testinglaboratories that the system is fail-safe under all operatingcircumstances.

FIG. 12 provides an indication of the conventional way manufacturers ofMOS gas sensors look at the effects of temperature and relativehumidity. The solid lines 416, 418, and 420 are relative humidities of95%, 65%, and 35% respectively. FIG. 12 illustrates the conventionalview that MOS sensors' Rs/Ro ratios (environmental dependencies) alongthe y-axis are functions of an infinite number of combinations ofrelative humidities and ambient temperatures. Therefore, theconventional approach to compensating for environmental dependencies isto use a microprocessor and digital lookup charts to compensateseparately for these influences. Besides the disadvantage of basing acritical safety system on a microprocessor and firmware, this method isonly an approximation—particularly at lower temperatures and relativehumidities.

The environmental uncertainties shown in FIG. 12 are caused byvariations in the air's water content as will later be shown inconnection with FIGS. 13-15. Manufacturer data includes multipledistinct slopes 416, 418, and 420 of interacting temperatures andrelative humidities. Slope 416 indicates temperature/humidity dependencyat 95 percent relative humidity, slope 418 indicatestemperature/humidity dependency at 65 percent relative humidity, andslope 420 indicates temperature/humidity dependency at 35 percentrelative humidity for a particular model sensor, namely the Figaro 821.The FIG. 12 data indicates the sensor's dependencies to temperature andrelative humidity according to the manufacturer of same.

FIG. 13 takes the average dew points found at various Rs/Ro values frommanufacturer-supplied data of FIG. 12 and plots them against thereciprocal of the Rs/Ro values. As can be seen from FIG. 13, a simplelinear function produces an excellent fit to the data points. As seen,the reciprocal of the Rs/Ro values were plotted. If a certain dew pointproduces an environmental Rs/Ro value of 0.800, an appropriatecompensation factor (K) for this model of sensor would be 1.25 (1/0.8).

Referring back to FIG. 12, the dashed slopes 422, 424, and 426 in FIG.12 are of fixed relative humidity, but they relate dew point (y-axis) totemperature (x-axis). Dashed slopes in FIG. 12 are supplied byapplicant, not by the manufacturer of the previously mentioned sensors.The close relationship of these dashed slopes to the manufacturersupplied slopes 416, 418, and 420, that separately consider temperatureand relative humidity, can be seen in FIG. 12.

FIG. 14 is a variation of the graph shown in FIG. 12. In FIG. 14, theRs/Ro ratios on the Y-axis have been replaced with dew points. Slope 428represents a relative humidity of 95 percent, slope 430 represents arelative humidity of 65 percent, and slope 432 represents a relativehumidity of 35 percent. For reference, three of the manufacturer's Rs/Roratios—0.9, 1.0, and 1.2—are superimposed over the data. Line 434represents a Rs/Ro ratio of 0.9, line 436 represents a Rs/Ro of 1.0, andline 438 represents a Rs/Ro of 1.2.

FIG. 15 shows the relationship of compensation factor vs. mass contentof water in air, the industry's metric. When the industry calculatescompensation factors, it measures water content in terms of grams percubic meter. This obscures the relationship between Rs/Ro environmentaldependencies and dew point because the relationship to g/m3 produces anearly straight line only when viewed on a log/linear graph. As shown inFIGS. 13-14, measuring water content in terms of dew point is a muchmore straightforward endeavor.

OPERATION

Therefore, in operation, a method of compensating MOS gas sensor 400comprises using MOS gas sensor 400 to provide a signal indicative of gasconcentration of a target gas (e.g., hydrogen) in an ambient (e.g., inthe plenum 290); providing a signal representative of dew point of theambient; and modifying the signal from the MOS gas sensor 400 using thesignal representative of dew point to simultaneously compensate for theeffects of both temperature and relative humidity. The signal from thegas sensor 400 is modified by the conditioning circuitry 402. In oneembodiment, the circuitry 402 comprises analog circuitry. The signalfrom the gas sensor is modified by the circuitry 402 using the signalrepresentative of dew point by transforming the dew point signal into alinear or semi-linear compensation factor and multiplying thatcompensation factor by the output of the sensor 400 (see FIG. 16). Forone model sensor, the Figaro TGS821 hydrogen sensor, the best fit forsensors with an average α of −0.725 is a simple y=ax+b lineartransformation, which is performed as follows: K=(A_(K)×t′)+B_(K), whereK is the dew point compensation factor (0.6619≦K≦1.463); t′ is dew pointin ° C., A_(K)=0.0109, and B_(K)=0.86352. K is a compensation factorbetween 0.6619 (−18.5° C. dew point) and 1.463 (55° C. dew point). Thisrange of compensation factors will compensate for environmental Rs/Rovalues ranging from 1.511 (the reciprocal of 0.6619) through 0.6835which is the lowest expected value for the fuel cell system 10 of theillustrated embodiment. In the preferred embodiment, the above-describedA_(K) and B_(K) coefficients are fixed constants of 0.0109 and 0.86352respectively and the signal representing the response slope of thesensor (which can range from −0.6 to −1.2) is normalized duringcalibration to an α of −0.725 before being compensated for the effectsof dew point. This is because the magnitude of required change in aparticular sensor's signal due to dew point is proportional to themagnitude of its response to hydrogen.

In an alternative embodiment, it is not necessary to normalize thesensor's gain to a specific alpha (such as −0.725) during calibration.This can be accomplished by instead scaling the influence of K factordepending on alpha. For alphas between −1.200 and −0.725, the effect ofK factor is accentuated, and for alphas between −0.600 and −0.725, theeffect of K factor is attenuated. This is accomplished with thefollowing function: Rcomp=10{circumflex over ( )}(Log(Rs)+(Log(K)/Ka)α).Here, “Rs” is the signal coming from the MOS sensor in terms ofresistance (Ω). The term “Ka” is the alpha value at which K factors wereoptimized for, in this case, where Ak=0.0109 and Bk=0.86352 are theterms used for converting dew point into K factors, Ka=−0.725. The term“α” is the alpha for that particular sensor. The term “Rcomp” is thesensor resistance (Ω) with the effects of environmental dependenciesnulled. Hydrogen concentration is then generated with a circuit (orsoftware) that performs the following function:w′=((Log(Rcomp/Ro)+2α/α). Here, the term w′ is the compensated hydrogenconcentration (PPM). “Ro” is the resistance (Ω) for that particularsensor at 100 PPM at a K factor of unity. For the TGS821, Ro istypically about 3.2 kΩ but can range from 1.0 kΩ to 10 kΩ.

In still another embodiment, the sensor's a need not be normalized to−0.725 during calibration and its response signal may be directly actedon by the dew point compensating circuitry. In one such embodiment, thecoefficients Ak and Bk are not constants and are instead variables thatare direct functions of alpha. Alternatively, improved accuracy acrossthe full range of α can be achieved by converting t′ into k using asecond-order polynomial transformation where the three coefficients Ak,Bk and Ck are variables that are direct functions of alpha. Otheralternatives are, of course, possible.

Thus, the circuitry 402 includes (see FIG. 16) an amplifier 440 which,in operation, multiplies t′ by A_(k), a summing amplifier or adder 442which, in operation, adds that product to B_(k) to produce the dew pointcompensation factor K, and a multiplier 444 which, in operation,multiplies the dew point compensation factor K by the output of thesensor 400. In one alternative embodiment, the functionality of thecircuitry 402 is implemented in digital circuitry instead of theillustrated analog circuitry. In another alternative embodiment, thefunctionality of the circuitry 402 is implemented in the controller 250.

Thus, a system has been provided for compensating a gas sensor for theeffects of temperature and relative humidity in a simplified fashion.

In compliance with the statute, the invention has been described inlanguage more or less specific as to structural and methodical features.It is to be understood, however, that the invention is not limited tothe specific features shown and described, since the means hereindisclosed comprise preferred forms of putting the invention into effect.The invention is, therefore, claimed in any of its forms ormodifications within the proper scope of the appended claimsappropriately interpreted in accordance with the doctrine ofequivalents.

What is claimed is:
 1. A method of compensating a MOS gas sensor,consisting of: using only a single MOS gas sensor to provide a signalindicative of gas concentration of a target gas in an ambient; providinga signal representative of dew point of the ambient; and modifying thesignal from the single MOS gas sensor using the signal representative ofdew point to simultaneously compensate for the effects of bothtemperature and relative humidity on the single MOS gas sensor.
 2. Amethod in accordance with claim 1 wherein modifying the signal from thegas sensor consists of using analog circuitry.
 3. A method in accordancewith claim 1 wherein modifying the signal from the gas sensor tocompensate for the effects of both temperature and relative humidityconsists essentially of using analog circuitry.
 4. A method inaccordance with claim 1 wherein providing a signal representative of dewpoint consists of measuring dew point.
 5. A method in accordance withclaim 1 wherein providing a signal representative of dew point consistsof measuring dew point using chilled-mirror equipment.
 6. A method inaccordance with claim 1 wherein providing a signal representative of dewpoint consists of deriving dew point from temperature and relativehumidity signals.
 7. A MOS gas sensor system consisting of: only asingle MOS gas sensor configured to provide a signal indicative of gasconcentration of a target gas in an ambient; and compensation circuitryconfigured to modify the signal from the single MOS gas sensor, using asignal representative of the dew point of the ambient, to simultaneouslycompensate for the effects of both temperature and relative humidity onthe single MOS gas sensor.
 8. A MOS gas sensor system in accordance withclaim 7 wherein the circuitry configured to modify the signal from thegas sensor consists of analog circuitry.
 9. A MOS gas sensor system inaccordance with claim 7 wherein the circuitry configured to modify thesignal from the gas sensor consists essentially of analog circuitry. 10.A MOS gas sensor system in accordance with claim 7 and furtherconsisting of hardware, coupled to the circuitry, and which isconfigured to determine dew point.
 11. A MOS gas sensor system inaccordance with claim 7 and further consisting of chilled-mirrorequipment which is configured to provide a signal representative of dewpoint, and which is coupled to the circuitry.
 12. A MOS gas sensorsystem in accordance with claim 7 and further consisting of: atemperature sensor configured to provide a signal representative oftemperature of the ambient; a relative humidity sensor configured toprovide a signal representative of the relative humidity of the ambient;and circuitry coupled to the compensation circuitry and which isconfigured to derive dew point from the temperature and humiditysignals.
 13. A method of compensating a MOS gas sensor, consisting of:using only a single MOS gas sensor which provides a signal indicative ofgas concentration of a target gas in an ambient; determining the dewpoint of the ambient; determining a compensation factor for the singleMOS gas sensor, and wherein the compensation factor is based upon thedetermined dew point; and modifying the signal from the single MOS gassensor using the compensation factor.
 14. A method in accordance withclaim 13 wherein the MOS gas sensor is of a given design, and whereindetermining a compensation factor consists of setting a compensationfactor based upon the given design of MOS gas sensor, as well as basedon the determined dew point.
 15. A method in accordance with claim 13wherein modifying the signal from the gas sensor consists of usinganalog circuitry.
 16. A method in accordance with claim 13 whereinmodifying the signal from the single MOS gas sensor to compensate forthe effects of both temperature and relative humidity consistsessentially of using analog circuitry.
 17. A method in accordance withclaim 13 wherein determining dew point consists of measuring dew point.18. A method in accordance with claim 13 wherein determining dew pointconsists of measuring dew point using chilled-mirror equipment.
 19. Amethod in accordance with claim 13 wherein determining dew pointconsists of measuring temperature and relative humidity and deriving dewpoint from the measured temperature and relative humidity.
 20. A MOS gassensor system consisting of; only a single MOS gas sensor configured toprovide a signal indicative of gas concentration of a target gas in anambient; equipment configured to determine the dew point of the ambient;and compensation circuitry configured to modify the signal from thesingle MOS gas sensor using a compensation factor, the compensationfactor being selected based upon the determined dew point.
 21. A MOS gassensor system in accordance with claim 20 wherein the single MOS gassensor is of a given design, and wherein the compensation factor is setbased upon the given design, as well as based upon the determined dewpoint.
 22. A MOS gas sensor system in accordance with claim 20 whereinthe compensation circuitry consists of analog circuitry.
 23. A MOS gassensor system in accordance with claim 20 wherein the compensationcircuitry consists essentially of analog circuitry.
 24. A MOS gas sensorsystem in accordance with claim 20 wherein the equipment configured todetermine the dew point of the ambient consists of chilled-mirrorequipment.
 25. A MOS gas sensor system in accordance with claim 20wherein the equipment configured to determine the dew point of theambient consists of a temperature sensor which, in operation, provides asignal representative of temperature of the ambient, a relative humiditysensor which, in operation, provides a signal representative of therelative humidity of the ambient, and circuitry coupled to thecompensation circuitry, which, in operation, derives dew point from thetemperature and humidity, signals.